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MQ-5B > System Overview > Flashcards

System Overview Flashcards

1
Q

What is the Aircrafts maximum takeoff weight

A

1950 pounds

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2
Q

How much approximate horsepower does each engine provide

A

56 hp

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3
Q

What is the engine displacement

A

800 cm³ or 0.8 L

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4
Q

How is the MQ –5B cooled

A

Liquid cooled 50/50 mix of water and glycol coolant

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5
Q

How is the power from the crankshaft transfer to the propellers

A

A centrical clutch transfers power from the crankshaft to the propeller through the propeller Drive assembly

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6
Q

What is the fuel capacity fuselage fuel tank

A

190+ or -5 L

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7
Q

What is the fuel capacity of the wing tanks

A

110+ or -5 L

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8
Q

Which electrical system components reduce 28 VDC to lower voltage required for other components

A

Converters

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9
Q

What the voltages do the converters outlet

A

15, -15, 12, & 5 VDC

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10
Q

Which component is the MQ – 5B Primary Attitude sensor

A

Primary sensor
INS Internal Navigation Sensor

Back up sensor
DMU Dynamic Measurement Unit

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11
Q

Which components is the MQ- 5B Primary altitude sensor

A

ADU Air Data Unit

Back up sensor

a. GPS Altitude
b. RPM Table

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12
Q

Which component is the MQ-5B Primary Airspeed sensor

A

ADU Air Data Unit

Back up sensor
Pitch table

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13
Q

Which component is the MQ – 5B Primary Heading sensor

A

INS internal navigation sensor

Back up sensor
FVU Flux valve unit

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14
Q

Which component is the MQ – 5B Primary Position sensor

A

INS/DGPS Internal Navigation Center/Differential Global Positioning System

Back up sensor

Back up DGPS differential global positioning system

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15
Q

Which component is the back up Heading sensor

A

FVU

Flux valve unit

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16
Q

Which component is the back up Position sensor

A

DGPS

Differential global position sensor

17
Q

Which component is the back up Attitude sensor

A

DMU

Dynamic measurement unit

18
Q

Which Component contains the auto pilot logic

A

MCPA modular central processing assembly

19
Q

How does the aircraft automatically make coordinated turns

A

ARI

Aileron Rudder Interconnect

20
Q

How far away Can the RVT to be from the aircraft and still receive video & telemetry

A

40 km

21
Q

Datalink system was designed to provide vacations between aircraft and ground antennas up to how many kilometers

A

277 km

22
Q

Which component is required for all parachute deployment

A

FTLU

Flight termination logic unit

23
Q

What are the basic components of the ERS

Emergency recovery system

A

Parachute, ordinance, FTLU, and MCPA

Flight termination logic unit

Modular central processor assembly

24
Q

How many and what type antennas are on the TGDT

A

3 - Directional, Omni, and GPS

25
Q

What is the range of the GDT primary directional antenna

A

277 km

26
Q

How many what type and what with cables connect a TGDT to an OSGCS

A

3-300 meter fiber optic cable single mode

27
Q

Which hazard awareness statement as you to prove it bodily injured or death

A

Warning

28
Q

Hazard awareness statement is used to prevent damage or destruction of equipment

A

Caution

29
Q

What is the minimum allowable distance between open flames or lit cigarette and a fuel source

A

50 feet

30
Q

How far away do personnel need to be if standing in line with a turning propeller

A

164 feet

31
Q

What type of Eye protection is required within 164 feet of turning propellers

A

ANSI Z87.1

32
Q

What location requires all personnel to wear safety shoes

A

Flightline

MQ-5B (1 decks)

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